Airworthiness Directive 98-24-11

recurring
Official AD 98-24-11 · FR doc 98-31011 · 1998-11-23 · airframe

Airworthiness Directives; Mooney Aircraft Corporation Models M20B, M20C, M20D, M20E, M20F, M20G, M20J, M20K, M20L, M20M, and M20R Airplanes

What this AD requires

This amendment adopts a new airworthiness directive (AD) that applies to certain Mooney Aircraft Corporation (Mooney) Models M20B, M20C, M20D, M20E, M20F, M20G, M20J, M20K, M20L, M20M, and M20R airplanes. This AD requires inspecting the aileron control links for the installation of a reinforcing gusset; and, if no gusset is installed, repetitively inspecting the aileron control links (left-hand and right-hand) for cracks. If cracks are found, this AD requires replacing the aileron control links with parts of improved design. This AD is the result of service difficulty reports (SDR's) on the aileron control links and reported failures of the aileron control links. The actions specified by this AD are intended to detect and correct cracked aileron control links, which could result in loss of aileron control with consequent loss of control of the airplane.

Repetitive inspection. Re-inspect every 100 hours. The next-due date/hours depend on this aircraft’s time in service — a records report computes it from the logbooks.

Which aircraft AD 98-24-11 applies to

MakesMooney
ModelsM20B, M20C, M20D, M20E, M20F, M20G, M20J, M20K, M20L, M20M, M20R, M20
Serial-conditional — narrows to serials 24-0001–24-3359, 25-0001–25-1999, 27-0001–27-0197, 29-0001–29-0042.

M20B, M20C, M20D, M20E, M20F, M20G, M20L: all serial numbers. M20J: s/n 24-0001 through 24-3359. M20K: s/n 25-0001 through 25-1999. M20M: s/n 27-0001 through 27-0197. M20R: s/n 29-0001 through 29-0042.

Whether AD 98-24-11 actually applies to your aircraft (by serial and installed parts) and whether it’s already complied with comes from that aircraft’s records.

How AD compliance is recorded

A valid compliance record (14 CFR 43.9) states:

Method of complianceThe specific action taken (inspected, replaced, modified) and to what revision.
DateWhen the work was done.
Aircraft timeTotal time in service / tach at compliance — how recurring next-due is computed.
Signature & certificateThe A&P/IA who returned it to service, with certificate number.
Is AD 98-24-11 complied with on your aircraft?

Tailplate reads a tail number’s logbooks and matches every applicable AD — including this one — to its compliance evidence, with recurring next-due dates computed.

Look up a tail number →Read the full directive (Federal Register)

Applicability is derived from the FAA directive corpus and is advisory, not a legal airworthiness determination. Compliance is established only from an aircraft’s actual records.